Numerical Study of Irregularly Roughened Micro-Particles’ Drag in Laminar Flow
The effect of surface roughness in laminar flow has been the focus of recent research related to drag reduction. However, although particle transport is governed by laminar flow in most applications, the effect of surface texture on the drag of a sphere has mostly been addressed in the transitional and turbulent regimes. The aim of the present study is to explore the drag behavior of rough spherical micro-particles in laminar flow. The spheres’ roughness has been structured based on a 3D complex Weaire–Phelan model, as well as on a simpler orthogonal lattice one, and quantified as per various definitions. The emerging surface roughness comprises irregular elements in terms of shape and size. The investigation has been performed at Reynolds numbers ranging from 2 to 8. The drag coefficient is found to drop quadratically with increasing roughness. Relative roughness can reduce the total drag on the particle by over 21%. The key physical mechanism is explained by the particles’ surface cavities, which contain recirculating, nearly stagnant fluid, thus creating a self-lubricating effect that reduces skin friction, as the main flow skims over the top without entering the cavities. A reduction in total drag arises when skin friction drag reduction is larger than the increase in form drag. Understanding the drag behavior of spherical particles with irregular surface texture provides new and useful insight into low Reynolds number transport phenomena related to a variety of engineering applications.
Authors
- Eleni Papazoglou
- Demetri Bouris (ORCID: https://orcid.org/0000-0003-3464-6945)
- Konstantinos-Stefanos Nikas (ORCID: https://orcid.org/0000-0003-2934-4811)
Institutions
- National Technical University of Athens (GR)
- University of West Attica (GR)
Publication Details
- Journal
- Applied Sciences
- Published
- 2025-08-18
- DOI
- https://doi.org/10.3390/app15169090
- Primary Topic
- Particle Dynamics in Fluid Flows
- Type
- article
- Field-Weighted Citation Impact
- 0.00